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Numerical mixing calculations of confined reacting jet flows in a cylindrical duct
Author(s) -
Victor L. Oechsle,
J. D. Holdeman
Publication year - 1995
Publication title -
33rd aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1995-733
Subject(s) - mechanics , combustor , body orifice , duct (anatomy) , nox , combustion , mixing (physics) , penetration (warfare) , materials science , orifice plate , mechanical engineering , physics , chemistry , engineering , medicine , pathology , quantum mechanics , organic chemistry , operations research
The results reported in this paper describe some of the main flow characteristics and NOx production results which develop in the mixing process in a constant cross-sectional cylindrical duct. A 3dimensional numerical model has been used to predict the mixing flow field and NOx characteristics in a mixing section of an RQL combustor. Eighteen configurations have been analyzed in a circular geometry in a fully reacting environment simulating the operating condition of -1 actual RQL gas turbine combustion liner. The evaluation trix was constructed by varying three parameters: 1) ,.-to-mainstream momentum-flux ratio (J), 2) orifice shape or orifice aspect ratio, and 3) slot slant angle. The results indicate that the mixing flow field and NOx production significantly vary with the value of the jet penetration and subsequently, slanting elongated slots generally improve the NOx production at high J conditions. Round orifices produce low NOx at low J due to the strong jet penetration. The NOx production trends do not correlate with the mixing non-uniformity parameters described herein.

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